page_title: Mil Mi-2
section_title: Specifications (Mi-2T)
hierarchical_section_title: Mil Mi-2 / Specifications (Mi-2T)
caption_attribution_description: Cockpit of Mil Mi-2. (Aviation Museum in Kosice, Slovakia)
context_page_description: The Mil Mi-2 is a small, lightly armed turbine-powered transport helicopter that could also provide close air support when armed with 57 mm rockets and a 23 mm cannon.
context_section_description: Data from Jane's All The World's Aircraft 1982–83
  General characteristics
  Crew: One
  Capacity: 8 passengers / 700 kg (1,543 lb) internal cargo / 800 kg (1,764 lb) external cargo
  Length: 11.4 m (37 ft 5 in)
  Height: 3.75 m (12 ft 4 in)
  Empty weight: 2,372 kg (5,229 lb)
  Gross weight: 3,550 kg (7,826 lb)
  Max takeoff weight: 3,700 kg (8,157 lb)
  Powerplant: 2 × PZL GTD-350P turboshaft engines, 300 kW (400 shp)  each
  Main rotor diameter:  14.5 m (47 ft 7 in)
  Main rotor area: 165.15 m² (1,777.7 sq ft) 
  Blade section: NACA 23012M
  Performance
  Maximum speed: 200 km/h (120 mph, 110 kn)
  Range: 440 km (270 mi, 240 nmi) (max internal fuel, no reserves)
  Service ceiling: 4,000 m (13,000 ft)
  Rate of climb: 4.5 m/s (890 ft/min)
  Disk loading: 22.41 kg/m² (4.59 lb/sq ft)
  Power/mass: 0.0806 kW/kg (0.0490 hp/lb)
caption: Cockpit of Mi-2 exhibited in Aviation Museum, Košice, Slovakia
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